Wind powered turbine engine

ABSTRACT

A wind turbine engine comprising rotor blades disposed within an outer casing and a half-spherical head located in front of the rotor blades and blocking the inner 50% of the radius of the rotor blades, the casing and head creating an acceleration chamber wherein incoming wind is speeded up and redirected around the head, and the accelerated wind then rotates the wind turbine rotor blades to generate power.

BACKGROUND OF THE INVENTION

The inventor has studied examples of present state of the art wind turbines of the propeller type. It was apparent that certain improvements could be made to harness a higher percentage of energy from a given cross section of wind accessed by their propeller blades. Based on principles of physics and aerodynamics known to the inventor, some serious possibilities and alternatives were apparent. At the present time, there is a growing demand for environmentally clean energy production. Costs of maintenance including the repair of weather damage to suburban and rural electrical distribution systems has reached the point where such systems are no longer profitable. This situation now provides adequate incentive toward the invention and development of more efficient and localized wind power electrical generation in the range of fifty kilowatts to one megawatt.

OBJECTS OF THE INVENTION

The inventor had determined that successful attainment of the following objects would lead to the development of a new type of wind power unit with a very high level of efficiency:

Firstly, to deal with the matter of recovering and harnessing wind energy not being captured by the inner fifty percent of the radius length of propeller blade systems as common to present state of the art wind turbines.

Secondly, to produce a wind power unit to more efficiently harness useable levels of energy from a broader range of wind speeds.

Thirdly, to create a wind power unit capable of recovering a maximum percentage of energy from the wind. In other words, can we build a wind power unit as efficient as steam and gas turbines?

Fourthly, to design and build a wind power unit which presents a lower or much less imposing cross section within its environment, or a combination of both.

BASIC DESCRIPTION AND IMPROVEMENTS OVER PRESENT STATE OF THE ART

Existing propeller turbine wind power units of present state of the art are not harnessing a very high percentage of energy from the cross section of wind addressed by such units. Three bladed propellers do not harness much of that energy. Present state of the art arrangements with larger numbers of blades might present some improvement within the scope of smaller sized systems. The inner 50% of the radius of propeller driven wind power systems is not harnessing much of the cross section of energy being addressed. The most practical solution to dealing with the inner 50% of the radius of propeller blades from their axle center, is to efficiently block off that area, and access the redirected energy with turbine blades extending radially beyond the blocked off area.

This invention, in its presently preferred embodiment, employs a spherical head arrangement, hereinafter referred to as a “speedball” in front of, and covering more than 50% of the radius from axle center to the outer tips of its turbine blades. The speedball increases the velocity of redirected wind energy, to more completely address a larger number of shorter turbine blades.

The amount of wind speed increase as the oncoming wind curves around the half spherical speedball head is theoretically, the equivalent of ¼ of the circumference of the spherical head, over its radius, to its center point, and that figure comes to 1.57 to 1. The significance of this is that available kinetic energy in a moving air mass at a given wind speed is a cubic function. This means that the net wind velocity increase, as recently confirmed by the inventor's engineers is 46%, after deducting drag factors. The resulting increase in available wattage of kinetic energy is 1.46 cubed, or about 311%. The inventor refers to the increase in available energy as “kinetic energy enhancement”. Present mathematical formulae for calculating watts per square meter of air in motion uses a standard mass or weight per cubic meter of air at a given altitude and temperature. The entire mathematical formula, to determine available watts per square meter in a moving air mass, as more particularly explained by the American Wind Energy Association, does not deal with compression. The inventor, however, is clearly aware that any compression of the oncoming air mass is going to increase its weight per cubic meter, to provide a further gain in available wattage per square meter, and that further gain would also be a cubic function. An example of the advantage of adding compression, would be where the compression factor would be 25%, increasing available watts per square meter to 1.25 cubed, which totals 1.953. As a consequence, we should have a further 95% as to available wattage per square meter. The inventor also refers to this method of increasing available kinetic energy per square meter as “kinetic energy enhancement”.

Present state of the art wind turbine systems tend to be limited as to the range of wind speeds from which they can harness a useful amount of wind energy. The spherical head arrangement increases the speed of the wind redirected from that inner 50% of the center to blade tip radius of the turbine rotor and blade assembly, but the faster moving wind is inclined to address only the inner radial portion of the turbine blades. To even out wind flow through the operating aperture containing the multi-bladed turbine rotor, a compound curved intake scoop arrangement is used to scoop inward a larger volume of incoming wind, toward the said shorter and more numerous turbine blades. This annular ring scoop is further designed with an inner facing airfoil arrangement, which increases the velocity of the captured wind, to much the same extent as that achieved by means of the said spherical head. The overall objective is to increase incoming wind speed, and then have this faster moving wind evenly address the aperture containing the larger number of shorter turbine blades. A further advantage of the said intake scoop, is that it captures an enlarged volume of oncoming wind, thereby creating compression, increasing the mass or weight of the wind column as it addresses the turbine blades, increasing the wattage of kinetic energy addressing the turbine blades. Through the combination of an extended length outer periphery airfoil extending rearward from the front outside edge of the said intake scoop, and an outward expansion proceeding to the rear behind the turbine rotor and blades assembly, a lower pressure or vacuum exhaust situation is achieved.

We now have a wind turbine engine, with supercharging at its intake, higher velocity and compression of wind mass entering the cylindrical encasement of its turbine rotor and blades, and with all of its blades adequately addressed to produce maximum torque.

This is followed by an exhaust area of continuously lowering pressure, behind the turbine rotor and blade assembly. All of the basic attributes of a turbine engine are now present within this embodiment. In the particular case of this wind turbine engine, its turbine blades will have blade pitch control. Where a 3-bladed wind turbine of present state of the art has its blades built to take advantage of aerodynamic lift, the short blades of this wind turbine engine must be shaped to harness more direct torque. Blade pitch control is considered essential in this embodiment, to most efficiently access a full range of wind speeds, as well as being able to set the turbine blades at full open neutral in the case of excessively high wind speeds, and at that point, the blades are then being more directly driven by aerodynamic lift, and continue to produce power. What is now readily apparent, is that with a much higher level of efficiency, we are now dealing with a situation where a wind turbine engine will be rather small in size, against its output potential, compared to wind turbines of present state of the art.

With this invention, we now have a new concept for engineers and other people skilled in the art to work with. A number of improvements will be made, as is usual, to the point where an absolute maximum amount of wind energy will be harnessed by future versions of this invention.

Although this preferred embodiment is primarily meant to serve as a wind energy harnessing device to operate within a range of 50 kilowatts to 1 megawatt, the inventor presently sees its upward range of output potential in the order of 5 megawatts. Those skilled in the art have already expanded three bladed propeller systems to where their largest wind turbines have 2½ megawatts of potential output. Future large versions of the present invention should be able to match that figure, and may ultimately double it.

The inventor anticipates some potential toward the use of special embodiments of this invention in water power and drive applications, and perhaps also with regard to high efficiency air circulating fan systems.

DETAILED DESCRIPTION

FIG. 1 is a partially cut away side view of a preferred embodiment of the invention, as mounted on the rotatable top of its support tower platform, with turbine rotor and twelve turbine blades, and with its wind intake scoop cross section cut away to show the rotor and turbine blades. Other details, being mechanical in nature, would be present state of the art, and do not need to be shown to illustrate the essential principles, details and novelty of the inventive concept.

FIG. 2 is a frontal view of the same wind turbine engine embodiment, as mounted on its rotatable tower top, illustrating its wind capture area, wind intake scoop, turbine blades, and airfoil covered support and reinforcement members for the wind intake scoop and internalized axle and drive system.

FIG. 3 is a rear view of the same wind turbine engine on top of its tower mounting, as it would look directly from the rear.

FIG. 4 is a side view of the wind turbine engine, on top of its tower mounting, as it would look directly from the side, (similar in appearance to a jet turbine engine) mostly enshrouded, or encapsulated by the extended airfoil shape of its wind intake scoop and flow through encasement assembly.

FIG. 5 is a simplified drawing of a three row blade system, as might be applied to the turbine rotor, and within the flow through and turbine drive chamber respectively, with one ring of 12 stabilizer blades being firmly mounted to the inside surface of the flow through and turbine drive chamber closely between two wind driven rows of turbine blades, as mounted and affixed to a single turbine rotor. The stabilizer blades serve to dampen or smooth out turbulence, and can enhance efficiency, when properly shaped and engineered.

With all of the foregoing in view, and such other and further purposes, advantages or novel features as may become apparent from consideration of this disclosure and specification, the present invention consists of the inventive concept which is comprised, embodied, embraced or included in various specific embodiments of such concept, reference being made to the accompanying figures, in which:

FIG. 1 is a partially cut away side view of a preferred embodiment of the invention, as mounted on the rotatable top of its support tower platform, where we have wind intake scoop and flow through encasement assembly 1, embodying s-curve velocity increasing surface 1 a, flow through and turbine drive chamber area surface 1 b, rearward expanding exhaust channel surface 1 c, and outer airfoil curved surface 1 d, to provide converging airflow to augment exhaust induction. Then we have half sphere wind displacement and velocity head 2, radially mounted airfoiled front end structural support members 3, for wind intake scoop and flow through encasement assembly 1, and also supporting the front end of encased axle/driveshaft (not shown), then we have turbine blades 4, as mounted on turbine rotor 5, then we have encasement body 6, for axle/driveshaft, mechanicals and electrical generator components, followed by rear structural support and reinforcement members 7, rotatable support table 8, for the entire wind turbine engine, along with its encasement and structural supports, which is mounted onto, and collared into the top end of support tower 9.

As a functional explanation, with recommendations toward achieving best wind turbine engine performance, we now refer to wind intake scoop and flow through encasement assembly 1, where its velocity increasing s-curved frontally projecting inner facing surface 1 a, is designed to provide essentially the same amount of velocity increase to incoming wind, as provided by wind displacement and velocity head 2. The inner facing surface of wind intake scoop and flow through encasement assembly 1, and the outer diameter of wind displacement and velocity head 2, can be spaced apart, or separated to an ideal level, where a tolerable amount of compression of the incoming wind mass is achieved, without seriously slowing down the said incoming wind mass. This is important, as there will be a balancing point of radial length of that separation distance, between achieving the most compression, limiting throughput wind speed reduction, or ultimately spilling off some of the incoming wind mass. Turbine blades 4, may not be able to handle an over compressed air mass fast enough, to maintain the smoothness of flow essential to greatest energy capture levels by means of the said turbine blades 4. Best available energy gain ratios provided by velocity increase and compression would not be achieved without the above described balancing procedure being carefully applied, with the best ratio assuring highest energy capture levels over a broad range of wind speed.

A further comment is also in order, where the wind turbine engine's turbine blades would be placed, contained and addressed within the outer 50% of the radius from axle centre to those blade tips. That could change somewhat, related to the foregoing balancing procedure. A properly balanced system of intake volume, velocity increase, and compression, is the most important consideration, and will harness the most energy per square meter.

FIG. 2 is a frontal view of the same wind turbine engine embodiment, where we have an unobstructed direct frontal view of wind intake scoop and flow through encasement assembly features, being s-curved intake scoop surface(s) 1 a, and outer airfoil surface 1 d, then speedball wind displacement and velocity head 2, front end structural support and reinforcement members 3, turbine blades 4, encasement body 6, rotatable support table 8, and the stationary top end of support tower 9.

What we are seeing here is quite similar to the frontal view of a jet turbine engine as one might observe on large passenger jet aircraft.

FIG. 3 is a rear view of the same wind turbine engine embodiment, Where we have an unobstructed direct rear view of wind intake scoop and flow through encasement assembly features, being internalized rearward expanding exhaust channel surface 1 c, and outer airfoil surface 1 d, then we have front end structural support members 3, turbine blades 4, encasement body 6, rear structural support members 7, rotatable support table 8, as mounted on the top end of support tower 9.

FIG. 4 is an unobstructed side view of the wind turbine engine, where we have wind intake scoop and flow through encasement assembly outer airfoil surface 1 d, encasement body 6, rear structural support members 7, then rotatable support table 8, as mounted on the top end of support tower 9.

FIG. 5 is a partially cut away side view of a second preferred embodiment of the invention, with two rows of twelve turbine rotor blades 4, and 11, mounted on its rearward extended drive rotor 5, where the said two rows of turbine blades are spaced some distance apart on the said rearward extended drive rotor 5, to properly position a fixed stationary non-rotating ring assembly of twelve flow stabilizer blades 10, with adequate clearance between said stabilizer blades assembly 10, and the two rows of turbine blades 4, and 11, and the said non-rotating ring of twelve flow stabilizer blades is affixed or solidly mounted to the inner circumference of extended flow through and turbine drive area surface 1 b. All other elements not essential to the placement of the two rows of turbine blades 4 and 11, with flow stabilizer blades 10, placed between the said two rows of turbine blades, on rearward extended rotor 5, are completely numbered, described and explained in FIGS. 1, 2 and 3 respectively. 

1-8. (canceled)
 9. A fluid turbine, comprising: a rotor and blade assembly, including: a rotor, the rotor being rotatable about a rotation axis; a plurality of blades, each of the blades having a tip, the blade tips defining a blade tip radius with respect to the rotation axis; a fluid displacement head arrangement blocking off at least 50% of the blade tip radius from the rotation axis towards the blade tips, the fluid displacement head arrangement shaped to redirect blocked-off fluid towards the blades extending radially beyond a blocked-off area.
 10. The fluid turbine of claim 9, further comprising: an annular fluid intake scoop and flow through encasement assembly surrounding the rotor and blade assembly, the encasement assembly having an interior surface and an exterior surface.
 11. The fluid turbine of claim 10, wherein the interior surface of the encasement assembly has a fluid velocity increasing surface forward of the blades, the fluid velocity increasing surface being shaped to increase the velocity of fluid entering the turbine.
 12. The fluid turbine of claim 11, wherein the fluid velocity increasing surface is S-shaped.
 13. The fluid turbine of claim 12, wherein the interior surface of the encasement assembly has an expanding exhaust channel surface rearward of the blades.
 14. The fluid turbine of claim 10, wherein the interior surface of the encasement assembly has an expanding exhaust channel surface rearward of the blades.
 15. The fluid turbine of claim 13, wherein the exterior surface of the encasement assembly is shaped to form an airfoil to provide converging airflow for augmenting exhaust from the turbine.
 16. The fluid turbine of claim 14, wherein the exterior surface of the encasement assembly is shaped to form an airfoil to provide converging airflow for augmenting exhaust from the turbine.
 17. The fluid turbine of claim 10, wherein the exterior surface of the encasement assembly is shaped to form an airfoil to provide converging airflow for augmenting exhaust from the turbine.
 18. The fluid turbine of claim 9, wherein the fluid displacement head arrangement is, at least in part, spherical.
 19. The fluid turbine of claim 10, wherein the fluid displacement head arrangement is, at least in part, spherical.
 20. The fluid turbine of claim 12, wherein the fluid displacement head arrangement is, at least in part, spherical.
 21. The fluid turbine of claim 14, wherein the fluid displacement head arrangement is, at least in part, spherical.
 22. The fluid turbine of claim 17, wherein the fluid displacement head arrangement is, at least in part, spherical.
 23. The fluid turbine of claim 10, wherein each of the blades has a controllable blade pitch.
 24. The fluid turbine of claim 10, further comprising a rotatable support constructed and arranged to permit the fluid turbine to be rotatably supported on a support tower.
 25. The fluid turbine of claim 10, wherein the blades are in two spaced-apart rows.
 26. The fluid turbine of claim 25, further comprising a plurality of flow stabilizers in between the rows of blades.
 27. The fluid turbine of claim 10, wherein the fluid turbine is a wind turbine.
 28. The fluid turbine of claim 10, wherein the fluid turbine is a water turbine. 